Aircraft ground support cart with component life optimization control

• US 7,412,840 B2
• Filed: 03/08/2005
• Issued: 08/19/2008
• Est. Priority Date: 03/08/2005
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Leathers, Thomas M.
• Primary Examiner(s): Tapolcai; William E.
• Application Number:
  US11/076,153
• Publication Number:
  US 20060201173A1
• Time in Patent Office: 1,260 Days
• Field of Search: 621/86, 622/36, 62/86, 62/79, 621/72, 622/37, 62208-209, 622/11
• US Class Current: 62/208
• CPC Class Codes: B64F 1/352 Mobile units
• CPC Class Codes: B64F 1/364 Mobile units
• CPC Class Codes: Y02T 50/80 Energy efficient operational measures, e.g. ground operations or mission management

Abstract

A ground-based system and method of supplying electrical power and temperature-controlled air to an aircraft environmental control system during ground support operations uses a throttle valve to control the flow of compressed air flowing through a heat exchanger. An air conditioner module mounted on a wheeled cart removes heat from the compressed air that is supplied to it from an auxiliary power unit (APU), and supplies cooled compressed air at a desired temperature. The temperature of the cooled compressed air is controlled by selectively positioning a throttle valve, which regulates compressed air flow from the compressed air source. The throttle valve position is controlled in response to one or more ambient meteorological conditions and/or the amount of electrical power being supplied from the system.

Claims

1. An aircraft ground cart for supplying electrical power and temperature-controlled air to an aircraft on the ground, the ground cart comprising:

an auxiliary power unit (APU) configured to (i) supply a flow of compressed air and (ii) generate electrical power;

an air conditioner module coupled to receive the flow of compressed air from the APU and configured, upon receipt thereof, to supply a flow of temperature controlled air;

a meteorological sensor configured to sense an ambient meteorological condition of an environment in which the ground cart is positioned and supply a meteorological signal representative thereof;

an electrical sensor configured to sense the electrical power generated by the APU and supply an output power signal representative thereof;

a control circuit coupled to receive the meteorological signal and the output power signal and operable, in response thereto, to supply a throttle valve control signal based at least in part on the meteorological signal and the output power signal; and

a throttle valve disposed between the APU and the air conditioner module, the throttle valve coupled to receive the throttle valve control signal and operable, in response thereto, to selectively move to control compressed air flow rate from the APU to the air conditioner module.

2. The ground cart of claim 1, wherein the meteorological sensor comprises a temperature sensor configured to sense ambient temperature of the environment in which the ground cart is positioned and supply a signal representative thereof.

3. The ground cart of claim 1, wherein the air conditioner module comprises:

a primary air flow passage coupled to receive a flow of primary air;

a compressed air flow passage coupled to receive the flow of compressed air; and

a first heat exchanger having at least a first fluid flow path and a second fluid flow path, the first fluid flow path fluidly coupled in series in the primary air flow passage, the second fluid flow path fluidly coupled in series in the compressed air flow passage, the first heat exchanger adapted to transfer heat between the primary air and the compressed air and supply at least conditioned compressed air,

wherein the throttle valve is mounted on the compressed air flow passage.

4. The ground cart of claim 3, further comprising:

at least one cooling turbine having an air intake port and an air exhaust port;

a second heat exchanger coupled to receive the conditioned compressed air from the first heat exchanger and turbine exhaust air from the cooling turbine air exhaust port, and adapted to transfer heat from the conditioned compressed air to the cooled air exhausted from the cooling turbine and supply warmed turbine exhaust air and further conditioned compressed air.

5. The ground cart of claim 4, wherein the cooling turbine air intake is coupled to receive the further conditioned compressed air from the second heat exchanger.

6. The ground cart of claim 3, further comprising:

a fan operable to draw the primary air from a primary air source into the primary air flow passage.

7. A support system for supplying electrical power and temperature-controlled air to an aircraft on the ground, the support system comprising:

an auxiliary power unit (APU) configured to (i) supply a flow of compressed air and (ii) generate electrical power;

an air conditioner module coupled to receive the flow of compressed air from the APU and configured, upon receipt thereof, to supply a flow of temperature controlled air;

an ambient temperature sensor configured to sense ambient temperature of an environment in which the ground cart is positioned and supply an ambient temperature signal representative thereof;

an electrical sensor configured to sense the electrical power generated by the APU and supply an output power signal representative thereof; and

a control circuit coupled to receive the ambient temperature signal and the output power signal and operable, in response thereto, to supply a throttle valve control signal based at least in part on the ambient temperature signal and the output power signal; and

a throttle valve disposed between the APU and the air conditioner module, the throttle valve coupled to receive the throttle valve control signal and operable, in response thereto, to selectively move to control compressed air flow rate from the APU to the air conditioner module.